US2027594A - Rotary compressor - Google Patents

Rotary compressor Download PDF

Info

Publication number
US2027594A
US2027594A US694232A US69423233A US2027594A US 2027594 A US2027594 A US 2027594A US 694232 A US694232 A US 694232A US 69423233 A US69423233 A US 69423233A US 2027594 A US2027594 A US 2027594A
Authority
US
United States
Prior art keywords
compression chamber
ports
rotary compressor
slots
chamber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US694232A
Inventor
Leslie R Huff
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ingersoll Rand Co
Original Assignee
Ingersoll Rand Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ingersoll Rand Co filed Critical Ingersoll Rand Co
Priority to US694232A priority Critical patent/US2027594A/en
Application granted granted Critical
Publication of US2027594A publication Critical patent/US2027594A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08Rotary pistons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/34Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
    • F01C1/344Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/30Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C18/34Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/30Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C18/34Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
    • F04C18/344Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member

Definitions

  • This invention relates to compressors, and more particularly to rotary compressors employing slidable vanes'for impelling the fluid from the inlet opening to the discharge opening of the compressor.
  • the objects of the invention are to retain the vanes in substantial sealing relationship with a compression chamber wherein they operate, to minimize the noise incident to the discharge of the compressed fiuid from the compression chamber, and to effect an adequate cooling of the compression chamber and the chambers wherewith it communicates.
  • Figure 1 is a longitudinal elevation, in section, of a rotary compressor constructed in accordance with tire practice of the invention and taken on the line through Figure 2,
  • Figure 2 is a transverse view taken on the line 2-2 of Figure 1 looking ,in the direction indicated by the arrows,
  • Figure 3 is a perspective view of a vane assembly
  • I Figure 4 is a view similar to Figure 1 taken through Figure 2 on the line 4-4 looking in the direction indicated by the arrows.
  • 20 designates, in general, a blower comprising a casing 2
  • a rotor 25 which is arranged eccentrically with respect to the compression chamber 22 and has an axial bore 26 into the ends of which are inserted trunnions or shafts 2'! and 28.
  • the shafts 21 and 23 are journaled in anti-friction bearings 29 seated in the heads 23 and may be keyed to the'rotor 25, as by means of pins 30.
  • Each shaft is provided with an externally threaded portion 3
  • the fluid intended to be compressed may be conveyed to the compressor by suitable piping (not shown) but which may open into an inlet chamber 33 having a plurality of branches 34 each one' of which terminates in a port 35 through which the fluid enters the compression chamber 22.
  • a discharge chamber 36 which, like the inlet chamber 33, has oblong branch chambers 31 into which the compressed fluid passes from a port or ports 33 communicating the chambers 31 with the compression chamber 22.
  • a series of ports 38 are arranged in spaced relation with respect to each other 10 and radially with respect to the compression chamber 22.
  • three such ports are shown, one each being arranged at the ends of the chambers 31 and one intermediate the ends.
  • Plugs 33 form closures-for certain of the ports 38.
  • the plugs 39 are threaded into the ports 38 and are, therefore, removable to enable the compressed fluid to be discharged less length than the length of the compression chamber 2
  • the edge of greater length of the 30 plates 42 bears against the wall of the compression chamber 22, and in the slots 40 is a complementary plate 44 having a diagonal surface to seat against the diagonal surface 43.
  • the plates 42 are so arranged that the diagonal surface 43 of one plate lies adjacent the end 46' of the other plate of a pair, thus preventing leakage of fluid over the narrow edges of the plates 44 which are of less height than the plates 42 to prevent contact thereof with the peripheral surface of the chaz ber 22.
  • the spacing of the slots may, however, be otherwise arranged but should be such "that no considerable number of adjacent slots are spaced equal distances apart.
  • a tube 48 leading from an oil container 49 is disposed in an axial bore 50 in the shaft 28 and extends into a similar bore 5
  • the portion of the tube 48 which extends into the shafts is journaled in bushings 52 which may be aflixed to the shaft, as by bracing.
  • In the wall of the tube are ports 53 through which oil passes into passages 54 opening into the bottoms of the slots 40.
  • the ports 53 are so arranged that they will be uncovered by the passages 54 only after completion of compression, thus preventing the entrance of compressed fiuid into the tube to check the flow of oil into the slots 40.
  • the compressor In order to assure rapid dissipation of the heat generated by compression the compressor is provided with a chamber 55 for cooling liquid.
  • the cooling liquid is introduced into the bottom defined .by arched walls 59 which extend outwardly in the direction of the main chambers 36 and 33. The air in passing through the chambers will thus be brought into contact with large areas of cooling surface to reduce the temperature of both the incoming and discharge fluid.
  • a rotary piston machine the combination with a cylindrical casing having an inlet and an outlet opening, of a rotary piston eccentrically arranged within the-casing, and of loose blades carried by and circumferentially spaced apart on the rotary piston for outward and inward movement, the circumferential distances between adjacent blades being not all equal.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)

Description

Jan. 14, 19360 R, HUFF ROTARY COMPRESSOR 3 Sheets-Sheet 1 Filed Oct. 19, 1953 INVENTOR.
4 la T UK UMW I $1 ImWW. Tw l l IHI Till% lmliww I g m HIS A TTORNEK Jan. 14, 1936. L. R. HUFF RoTAfiY COMERESSOR Filed Oct. 19, 1933 3 Sheets-Sheet 5 INVENTOR. ll
u ff.
.Lea ieR HIS ATTORNEY Patented Jano 14, 1936 a PTEQNT OFFICE ROTARY COMPRESSOR Leslie R. Huff, Phillipsburg, N. J., assignor to Ingersoll-Rand Company, Jersey City, N. J., a corporation of New Jersey Application October 19, 1933, Serial No. 694,232
2 Claims.
This invention relates to compressors, and more particularly to rotary compressors employing slidable vanes'for impelling the fluid from the inlet opening to the discharge opening of the compressor.
The objects of the invention are to retain the vanes in substantial sealing relationship with a compression chamber wherein they operate, to minimize the noise incident to the discharge of the compressed fiuid from the compression chamber, and to effect an adequate cooling of the compression chamber and the chambers wherewith it communicates.
Other objects will be in part'obvious and in part pointed out hereinafter.
In the drawings illustrating the invention and in which similar reference numerals refer to similar parts,
Figure 1 is a longitudinal elevation, in section, of a rotary compressor constructed in accordance with tire practice of the invention and taken on the line through Figure 2,
Figure 2 is a transverse view taken on the line 2-2 of Figure 1 looking ,in the direction indicated by the arrows,
Figure 3 is a perspective view of a vane assembly, and I Figure 4 is a view similar to Figure 1 taken through Figure 2 on the line 4-4 looking in the direction indicated by the arrows.
Referring more particularly to the drawings, 20 designates, in general, a blower comprising a casing 2| bored to form a compression chamber 22 of which the ends are closed by heads 23 secured to the casing 2| in any suitable manher, as by bolts 24.
Within the compression chamber 22 is-a rotor 25 which is arranged eccentrically with respect to the compression chamber 22 and has an axial bore 26 into the ends of which are inserted trunnions or shafts 2'! and 28. The shafts 21 and 23 are journaled in anti-friction bearings 29 seated in the heads 23 and may be keyed to the'rotor 25, as by means of pins 30.
Each shaft is provided with an externally threaded portion 3| for the accommodation of a nut acting against the outer end of the bearings 29, and the shaft 21 difiers from the shaft "28 only in that it is provided with an extension 32 whereby it may be coupled to a prime mover (not shown).
The fluid intended to be compressed may be conveyed to the compressor by suitable piping (not shown) but which may open into an inlet chamber 33 having a plurality of branches 34 each one' of which terminates in a port 35 through which the fluid enters the compression chamber 22. In the opposite side of the casing 2| is a. discharge chamber 36 which, like the inlet chamber 33, has oblong branch chambers 31 into which the compressed fluid passes from a port or ports 33 communicating the chambers 31 with the compression chamber 22.
Preferably, a series of ports 38 are arranged in spaced relation with respect to each other 10 and radially with respect to the compression chamber 22. In the present instance three such ports are shown, one each being arranged at the ends of the chambers 31 and one intermediate the ends. Plugs 33 form closures-for certain of the ports 38. The plugs 39 are threaded into the ports 38 and are, therefore, removable to enable the compressed fluid to be discharged less length than the length of the compression chamber 2| and having, at one end, a diagonal surface 43. The edge of greater length of the 30 plates 42 bears against the wall of the compression chamber 22, and in the slots 40 is a complementary plate 44 having a diagonal surface to seat against the diagonal surface 43. Thus when the rotor 25 is in operation the plates 42 35 and 44 are actuated centrifugally outwardly and the plate 44 will, by its :action against, the plate 42, cause the opposite end 46 of the plate 42 to be maintained in sealing relationship with the adjacent surface 41 of the head '23.
In their assembled positions the plates 42 are so arranged that the diagonal surface 43 of one plate lies adjacent the end 46' of the other plate of a pair, thus preventing leakage of fluid over the narrow edges of the plates 44 which are of less height than the plates 42 to prevent contact thereof with the peripheral surface of the chaz ber 22.
One objectionable feature in devices of this character, as heretofore constructed, has been 50 that of the noise incident to the discharge of the compressed fluid through the discharge ports into the discharge chamber. In practice I have found that such noise is due largely to the equal spacing of the vanes 4| and a conse-.
ments in the spaces between the slots located in a quadrant. The spacing of the slots may, however, be otherwise arranged but should be such "that no considerable number of adjacent slots are spaced equal distances apart.
To the end that the surfaces of the vanes and the slots 40, whereby they are guided, may be adequately lubricated a tube 48 leading from an oil container 49 is disposed in an axial bore 50 in the shaft 28 and extends into a similar bore 5| in the shaft 21. The portion of the tube 48 which extends into the shafts is journaled in bushings 52 which may be aflixed to the shaft, as by bracing. In the wall of the tube are ports 53 through which oil passes into passages 54 opening into the bottoms of the slots 40. The ports 53 are so arranged that they will be uncovered by the passages 54 only after completion of compression, thus preventing the entrance of compressed fiuid into the tube to check the flow of oil into the slots 40.
In order to assure rapid dissipation of the heat generated by compression the compressor is provided with a chamber 55 for cooling liquid.
The cooling liquid is introduced into the bottom defined .by arched walls 59 which extend outwardly in the direction of the main chambers 36 and 33. The air in passing through the chambers will thus be brought into contact with large areas of cooling surface to reduce the temperature of both the incoming and discharge fluid.
I claim:
1. In a rotary piston machine the combination with a cylindrical casing having an inlet and an outlet opening, of a rotary piston eccentrically arranged within the-casing, and of loose blades carried by and circumferentially spaced apart on the rotary piston for outward and inward movement, the circumferential distances between adjacent blades being not all equal.
2. In a rotary piston machine as claimed in claim 1, the arrangement that the spacing of the blades varies irregularly and the tips of the blades bear against the casing-inside by centrifugal force.
LESLIE R. HUFF.
US694232A 1933-10-19 1933-10-19 Rotary compressor Expired - Lifetime US2027594A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US694232A US2027594A (en) 1933-10-19 1933-10-19 Rotary compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US694232A US2027594A (en) 1933-10-19 1933-10-19 Rotary compressor

Publications (1)

Publication Number Publication Date
US2027594A true US2027594A (en) 1936-01-14

Family

ID=24787960

Family Applications (1)

Application Number Title Priority Date Filing Date
US694232A Expired - Lifetime US2027594A (en) 1933-10-19 1933-10-19 Rotary compressor

Country Status (1)

Country Link
US (1) US2027594A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2541405A (en) * 1946-12-18 1951-02-13 Bowser Inc Rotary hand pump
US2714858A (en) * 1950-11-03 1955-08-09 Kepka Frank Rotary compressors or pumps, in combination with hydraulic controls, and mechanical controls in co-ordination therewith
US3113526A (en) * 1961-04-13 1963-12-10 Nsu Motorenwerke Ag Slit apex seals
US3120921A (en) * 1961-07-25 1964-02-11 Royalty Holding Corp Automatically adjusting and compensating seal means for rotary machines
US3127096A (en) * 1964-03-31 Froede
US3291384A (en) * 1965-09-15 1966-12-13 Frisk Company Rotary compressor
US3827833A (en) * 1971-03-04 1974-08-06 Kawasaki Heavy Ind Ltd Rotor cooling device in an oscillation type compressor
US3999905A (en) * 1975-11-17 1976-12-28 Caterpillar Tractor Co. Rotary mechanism
US4468180A (en) * 1982-05-21 1984-08-28 Diesel Kiki Co., Ltd. Vane compressor having intermittent oil pressure to the vane back pressure chamber
US4850827A (en) * 1986-08-18 1989-07-25 Wankel Gmbh Cooling system of an eccentric shaft of a rotary piston internal combustion engine

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3127096A (en) * 1964-03-31 Froede
US2541405A (en) * 1946-12-18 1951-02-13 Bowser Inc Rotary hand pump
US2714858A (en) * 1950-11-03 1955-08-09 Kepka Frank Rotary compressors or pumps, in combination with hydraulic controls, and mechanical controls in co-ordination therewith
US3113526A (en) * 1961-04-13 1963-12-10 Nsu Motorenwerke Ag Slit apex seals
US3120921A (en) * 1961-07-25 1964-02-11 Royalty Holding Corp Automatically adjusting and compensating seal means for rotary machines
US3291384A (en) * 1965-09-15 1966-12-13 Frisk Company Rotary compressor
US3827833A (en) * 1971-03-04 1974-08-06 Kawasaki Heavy Ind Ltd Rotor cooling device in an oscillation type compressor
US3999905A (en) * 1975-11-17 1976-12-28 Caterpillar Tractor Co. Rotary mechanism
US4468180A (en) * 1982-05-21 1984-08-28 Diesel Kiki Co., Ltd. Vane compressor having intermittent oil pressure to the vane back pressure chamber
US4850827A (en) * 1986-08-18 1989-07-25 Wankel Gmbh Cooling system of an eccentric shaft of a rotary piston internal combustion engine

Similar Documents

Publication Publication Date Title
US2027594A (en) Rotary compressor
US2216053A (en) Rotary pump of the single rotor type
US3016184A (en) Rotary compressors
US2832293A (en) Vane pump
US2136117A (en) Rotary compressor, exhauster, pump, and the like
US1913758A (en) Rotary pump
US1697041A (en) Variable-capacity pump
US1499056A (en) Centrifugal pump
US1979621A (en) Balanced turbulence pump
US2042533A (en) Rotary pump, blower, or compressor and the like
US901539A (en) Multiple-stage air-compressor.
US1936935A (en) Combined rotary and reciprocating pump
US2189969A (en) Fluid pressure pump of thermicdynamical action
US2050533A (en) Oiling device
US1670229A (en) Combined variable-capacity and constant-volume pump
US2200198A (en) Vacuum pump
US2733663A (en) Deep well pumping apparatus
US1676103A (en) Lubricating and sealing system for rotary compressors
US2013078A (en) Centrifugal pump
US1676783A (en) Rotary pump
US1683962A (en) Pump
US1590384A (en) Refrigerating apparatus
US1136756A (en) Rotary pump.
US2004958A (en) Rotary pump
US2968252A (en) Engine